Accession Number:

AD0606557

Title:

Total Impulse Measuring System for Solid Propellant Rocket Engine: Phase II Report

Descriptive Note:

Corporate Author:

ROCKETDYNE CANOGA PARK CA

Personal Author(s):

Report Date:

1964-08-01

Pagination or Media Count:

49.0

Abstract:

Discussion and results of the two main considerations comprising the intermediate Phase II effort are presented 1 fabrication and test of the component parts of the system prior to their inclusion in the system and 2 assembly and test of the complete measurement system prior to its delivery to EAFB. Specific results of these separate but related program efforts are, respectively 1 source inspections and tests, where needed, to determine compliance with Rocketdyne drawings and specifications, and 2 alignment measurements and detailed tests to determine that the overall system peerformance conformed to the contractual requirement of 0.1 accuracy.

Subject Categories:

  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE